Space Research 1978
DOI: 10.1016/b978-0-08-022021-5.50060-4
|View full text |Cite
|
Sign up to set email alerts
|

Electron Temperature in the Equatorial E Region Measured by Two Rocket Experiments and by Incoherent Scatter

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

1
2
0

Year Published

1981
1981
2015
2015

Publication Types

Select...
6
1

Relationship

0
7

Authors

Journals

citations
Cited by 10 publications
(3 citation statements)
references
References 8 publications
1
2
0
Order By: Relevance
“…However, even when an electrode with a clean surface is used (Hirao & Oyama 1972;Oyama & Hirao 1976;Oyama et al 2008a, b) or another instrument is used whose measurement is not influenced by electrode contamination, the measurements still show T e to be higher than T n during the daytime. The T e value measured by a resonance cone instrument agrees with this measurement (Piel et al 1992), as well as that obtained by incoherent scatter radar (Smith et al 1978). Electron temperature inside and/or around the sporadic E layer (E s ) is controversial.…”
Section: E Regionsupporting
confidence: 73%
“…However, even when an electrode with a clean surface is used (Hirao & Oyama 1972;Oyama & Hirao 1976;Oyama et al 2008a, b) or another instrument is used whose measurement is not influenced by electrode contamination, the measurements still show T e to be higher than T n during the daytime. The T e value measured by a resonance cone instrument agrees with this measurement (Piel et al 1992), as well as that obtained by incoherent scatter radar (Smith et al 1978). Electron temperature inside and/or around the sporadic E layer (E s ) is controversial.…”
Section: E Regionsupporting
confidence: 73%
“…The high T e below the height of 98 km is considered to be due to the aerodynamical heating. The comparison of T e measurement was also conducted in US with an ac probe which was invented by Smith et al (1978), with good agreement. Figure 15 summarizes the results of the T e measurement by ETP when the rocket is in the center of Sq current system.…”
Section: Comparison With Other Probesmentioning
confidence: 92%
“…ETP has been flown in more than 50 Japanese sounding rockets including ones from the Showa Antarctica station (Hirao and Oyama, 1980;Schlegel et al, 1983). ETP was also deployed in the Copyright c TERRAPUB, 2013. sounding rockets of India, Brazil, USA, and West Germany with great success (Sampath et al, 1974;Smith et al, 1978;Schlegel and Oyama, 1987;Wilhelm et al, 1987;Piel et al, 1988Piel et al, , 1991Piel et al, , 1992Rohde et al, 1993). The probe was installed in 5 Japanese satellites: TAIYO (Oyama and Hirao, 1975), HINOTORI , KYOKKO (Oyama and Schlegel, 1984), OHZORA Oyama and Abe, 1987), and AKEBONO (Oyama, 1994).…”
Section: Introductionmentioning
confidence: 99%